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公开(公告)号：EP3396146A1
公开(公告)日：2018-10-31
申请号：EP16894475.9
申请日：2016-06-22
发明人： HIROKANE, Mariko , ANDO, Keisuke , UENO, Yoshihiko
CPC分类号： F02K7/10 , F02C7/00 , F02C7/057 , F02C7/26 , F05D2210/33 , F05D2220/10 , F05D2240/35 , F05D2250/51 , F05D2270/3061 , F23R3/10 , F23R3/20 , F23R3/22 , F23R3/28 , F23R2900/00015
摘要： A jet engine is provided with an inlet 11 for taking in air, and a combustor 12 that has a fuel injection port 30a for injecting fuel. The combustor 12 uses the air to combust the fuel injected from the fuel injection port 30a. Between the fuel injection port 30a and the rear end 15 of the inlet, the combustor 12 has a separation part 14 that defines an air flow path FA, through which air flows. A plurality of turbulence generating parts (20, 25) that cause the flow of air to be turbulent are disposed on the separation part 14. Each of the turbulence generating parts (20, 25) includes a member (21, 22, 25B) that, by moving or disappearing, can inhibit the turbulence of the flow of air. A drop in the thrust of the jet engine resulting from a high-pressure region reaching the inlet can thus be prevented.
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公开(公告)号：EP3401295A1
公开(公告)日：2018-11-14
申请号：EP16890647.7
申请日：2016-11-17
发明人： KURIMURA, Takayuki , MATSUMOTO, Mineaki , TSURU, Yasuhiko , NISHIKAWA, Kosuke , HIROKANE, Mariko
CPC分类号： F23M5/00 , C04B37/003 , C04B2237/38 , C04B2237/765 , C04B2237/80 , F01D25/00 , F02C7/00 , F16B7/00 , F16B11/00 , F16L13/08 , F16L13/10 , F16L23/16 , F16L49/00 , F23R3/42
摘要： Provided is a joined structure that has joining sections 15 in which a plurality of tubular bodies 11, 12 formed of a ceramic-based composite material are joined with each other via intermediate materials 16 by abutting end surfaces 11B, 12A of the tubular bodies, wherein the end surfaces 11B of the tubular body 11 are inclined so as to protrude from inner surfaces 11D of the tubular body 11 toward outer surfaces 11C thereof, and the end surfaces 12A of the tubular body 12 are inclined so as to protrude from outer surfaces 12C of the tubular body 12 toward inner surfaces 12D thereof.
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公开(公告)号：EP3396145A1
公开(公告)日：2018-10-31
申请号：EP16894474.2
申请日：2016-06-22
发明人： HIROKANE, Mariko , ANDO, Keisuke , UENO, Yoshihiko
CPC分类号： F23R3/28 , F02C7/00 , F02C7/26 , F02K7/10 , F05D2220/10 , F05D2240/35 , F23R3/10 , F23R3/20 , F23R3/42 , F23R2900/00015
摘要： A jet engine is provided with an inlet 11 and a combustor 12 having a fuel injection port 30a. The combustor 12 has a wall part 16 that defines an air flow path FA. The wall part 16 has a ramp part 60, which has an inclined face 62, and a first wall face 17 extending to the front-side end of the inclined face 62. The fuel injection port 30a is positioned at the ramp part 60. The inclination angle θ relative to the first wall face 17 of the inclined face 62 is at least 13.5 degrees. The height by which the ramp part 60 protrudes from the first wall face 17 does not exceed one fifth of the height of the inlet of the combustor 12. Thus provided are a jet engine and a flying object in which the inclination angle of the inclined face of a ramp is made larger so as to promote the mixing of fuel and air and to allow for stable flame holding at the rear of the ramp.
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公开(公告)号：EP3396146B1
公开(公告)日：2020-05-27
申请号：EP16894475.9
申请日：2016-06-22
发明人： HIROKANE, Mariko , ANDO, Keisuke , UENO, Yoshihiko
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公开(公告)号：EP3396145B1
公开(公告)日：2020-05-27
申请号：EP16894474.2
申请日：2016-06-22
发明人： HIROKANE, Mariko , ANDO, Keisuke , UENO, Yoshihiko
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